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vector
说明: 电机矢量控制仿真(svpwm方法)实测有效 包括坐标变换(vector control The simulation of motor vector control (SVPWM) includes coordinate transformation)
- 2021-02-08 20:09:38下载
- 积分:1
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IEEE33节点
采用simulink搭建IEEE标准33节点仿真模型及.m程序(IEEE standard 33 node simulation model)
- 2021-04-10 15:48:58下载
- 积分:1
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Laplace
说明: 求解二维拉普拉斯方程的matlab程序的实现(Solving two-dimensional Laplace equation)
- 2019-03-08 17:34:32下载
- 积分:1
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滑模第三版-上部仿真程序
滑模变结构 刘金坤 ,很好用,很实用,特别是机器人控制方向。(sliding mode control liujinkun)
- 2018-01-29 14:13:35下载
- 积分:1
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NS_SAR_ADC_1order
说明: 基于文章A 90-MS/s 11-MHz-Bandwidth 62-dB SNDR Noise Shaping SAR ADC的基本功能建模,仿真一阶噪声整形的噪声传输函数(Based on the basic function model of article , A 90-MS/s 11-MHz-Bandwidth 62-dB SNDR Noise Shaping SAR ADC , the noise transfer function of first-order noise shaping is simulated.)
- 2019-02-20 09:24:48下载
- 积分:1
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UPFC模型
说明: UPFC模型,模型非常详细和系统,有助于理解潮流控制器(UPFC model, which is very detailed and systematic, helps to understand power flow controllers)
- 2019-04-22 18:56:05下载
- 积分:1
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周期边界条件
说明: 周期边界,通过python代码实现,abaqus多尺度仿真,有效性能计算,复合材料(Periodic boundary, implemented by Python code, ABAQUS multi-scale simulation, effective performance calculation, composite materials)
- 2020-02-03 16:00:05下载
- 积分:1
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圣维南方程(洪水)
基于matlab 编程,利用一维圣维南方程组,模拟洪水演进过程(Using one-dimensional Saint-Venant equations to simulate flood routing process)
- 2021-04-12 09:48:57下载
- 积分:1
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djd
说明: 本模型采用abaqus自带的connector连接单元建模,实现了钉节点的模拟(In this model, the connector unit of ABAQUS is used to simulate the nail node)
- 2020-11-04 19:49:51下载
- 积分:1
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chapter5attitude
说明: 卫星姿态是指卫星星体在轨道上运行所处的空间指向状态。将直角坐标系的原点置于星体上,指向地面的Z轴反映偏航方向,Y轴反映俯仰方向,X轴反映滚动方向。星体在高空中沿局部地球铅垂方向和轨道矢量方向运行,不时地产生对三轴的偏移。姿态控制是通过姿态控制分系统(ACS)来实现,使用地平扫描仪可感应俯仰和滚动轴的姿态误差,使用速度陀螺仪和罗盘可感应偏航轴的姿态误差。(Satellite attitude refers to the spatial orientation of a satellite in orbit. The origin of the Cartesian coordinate system is placed on the star, the Z axis pointing to the ground reflects the yaw direction, the Y axis reflects the pitching direction, and the X axis reflects the rolling direction. The stars move along the direction of the earth's vertical direction and the orbit vector in the high altitude, resulting in the deviation of the three axis from time to time. Attitude control is realized by attitude control subsystem (ACS). The attitude error of pitch and rolling axis can be induced by using horizon scanner, and the attitude error of yaw axis can be induced by using speed gyroscope and compass.)
- 2017-10-29 16:46:09下载
- 积分:1